Optimal solid shells for non-linear analyses of multilayer composites. I. Statics

Author:

Vu-Quoc L.,Tan X.G.

Publisher

Elsevier BV

Subject

Computer Science Applications,General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference55 articles.

1. EAS-elements for 2-dimensional, 3-dimensional, plate and shell structures and their equivalence to HR-elements;Andelfinger;I. J. Numer. Methods Engrg.,1993

2. Refined shear-deformation models for composite laminates with finite rotations;Basar;I. J. of Solids Struct.,1993

3. G.P. Bazeley, Y.K. Cheung, B.M. Irons, O.C. Zienkiewicz, Triangular elements in bending–conforming and non-conforming solutions, Conference of matrix methods in structural mechanics, Air Force Inst. Tech., Wright-Patterson AF base, OH, 1965

4. An assumed strain approach avoiding artificial thickness straining for a non-linear 4-node shell element;Betsch;Commun. Numeri. Methods Engrg.,1995

5. A non-linear extensible 4-node shell element based on continuum theory and assumed strain interpolations;Betsch;J. Nonlin. Sci.,1996

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